| dc.creator |
Walton, J. |
|
| dc.date |
2013-06-26T10:52:34Z |
|
| dc.date |
2013-06-26T10:52:34Z |
|
| dc.date |
1957-11 |
|
| dc.date.accessioned |
2022-05-09T10:17:23Z |
|
| dc.date.available |
2022-05-09T10:17:23Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7978 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4783 |
|
| dc.description |
COA report 109 describes Flight Tests carried out on a swept back half wing of double elliptical section to investigate the nature of the boundary layer flow, with particular reference to Bounday Layer Instability and subsequent transition. |
|
| dc.description |
M.O.S. contract No. 6/ Aircraft/14002/C.B.6 (a) |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Report |
|
| dc.relation |
109 Addendum |
|
| dc.title |
Addendum to a theoretical and experimental study of the boundary layer flow on a 45 degrees swept back wing |
|
| dc.type |
Report |
|